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A STUDY OF CHARGE INJECTION IN 
ITO/PEDOT/MEH-PPY/Ca/Al PLEDs 

AND 

LIFT-OFF PROCESS IN POSITIVE PHOTO RESIST 

A Thesis Svbmitted 
In 

Partial Fulfillment of the Requirements 
For the Degree of 

Master of Technology 

By • 

TALARI MANTOJAYA 



To the 

DEPARTMENT OF ELECTRICAL ENGINEERING 
INDIAN INSTITUTE OF TECHNOLOGY, KANPUR 


AUGUST, 2005 



CERTIFICATE 


This is to certify that the work contained in the thesis entitled “A STUDY OF 
CHARGE INJECTION IN ITO/PEDOT/MEH-PPV/Ca/Al PLEDs AND LIFT-OFF 
PROCESS IN POSITIVE PHOTO RESIST’ by Talari Manojaya (Roll No. Y3 104 102) 
has been done under our supeivision and this work has not been submitted elsewhere 
for a degree. 




Dr. Baquer Mazhari 
Associate Professor 




Dr.Uitendra Narain 
Chief Research Engineer 


Department of Electrical Engineering 
Indian Institute of Technology 
Kanpur-208016 

j.* 




LI 2 SEP ZOOS 1^^ 


|wm*r •r- . ^i'^'TPT ^■?TSWX <|!STWI* 
«TTOfVir ar^Mir^'t ?r^«rT5T 



A cknowledgement 


I would like to thank my thesis supervisors Dr.J.Narain & Dr.Baquer Mazhari for 
provided me the opportunity to work in a cutting edge technology in the field of 
Organic Electronics. I was enormously admired by the deeper concepts of organic 
electronics when Dr.B.mazhari & Dr.Vasudha Bhatia taught us Organic Electronics and 
Material and Display Technologies respectively. DrJ.Narain and Dr.Asha Awasthi 
patience and efforts to fabricate devices and explain things clearly, in a simple manner, 
helped in making this thesis an exciting venture for me. I would also like to thank to 
Dr.Raghubhir Singh Anand for encouraging me all the time. 

I am indebted to the Department of Electrical Engineering & Samtei Center, IIT 
Kanpur for providing the opportunity and facilities for the thesis work & studies. I 
would like to thank Head of the department, all the faculty members and staff of 
electrical engineering, IIT Kanpur; for their help and guidance during my stay here. 

I am indebted to my fellow students, Gaurav.C, Bodhraj.G, Chander Pal, Ravi 
Kumar .M.N & Mahesh Kumar Reddy, these two years of staying arid working together 
have been a real delight. I thank to my B.Tech Colleagues and fiiends, P.Praveen 
kumar Reddy, A.Nageshwar, A.Narsimha, T.Vijay prakesh, P.Rajendra Prasad, Shiva 
Prasad, Sridhar.A, Naveen Goud, P.Balraj and Ram Mohan for encouraging me all the 
times. I also thank to my friends Mr.Srinivas Reddy, Sanjeev, Ratna Kumari, & Anil 
Kumar. 

I also thank to semiconductor laboratory associates, Sheetal Barai, Anand Biswas, 
Swapnil, Ramesh, Ramnath and Anjali Giri. 

In the end I would like to thank my parents and siblings for being a constant support 
during my whole course work. 


Talari Manojaya 



ABSTRACT 


To meet the challenges of the PLED technology, we have made an attempt to find the 
nature of currents in the ITO/PEDOT/MEH-PPV/Ca/Al device. Hole only devices are 
fabricated to observe the dependence of hole current on the thickness of the injection 
layer in the device with gold as cathode. A similar study has been done for electron only 
device with magnesium as anode. Both the studies provide the necessary information to 
design a device having a better charge balance which ultimately leads to improvement in 
efficiency. We had also made an attempt to optimize Lift-Off:- Image reversal process 
with positive photoresist for display application. 



Dedicated To 


My Father 


(Shri Narsimlu Talari) 



Contents 


Front page 

Certificate 

Acknowledgement 

Abstract 

Dedication 

Contents 

List of Figures 

Abbreviations and symbols 

Physical constants 

PART:-I 


I 

II 

III 

IV 

V 

VI 
EX 

xm 

XV 


1 . 


Introduction 


1-7 


1.1 

1.2 

1.3 

1.4 

1.5 

1.6 


Review 

Brief historical overview of electroluminescence diodes 
Conjugated polymers 

Excitations in organic semiconductors:- polarons and exicitions 

Summary 

Thesis Layout 


1 

2 
2 

4 

6 

7 


2. Physics of Charge injection and Charge transport 8-19 


2. 1 General Introduction of OLED 

2.2 Interface Barriers and Charge Injection 

2.3 Charge Transport 
2.3a Ohms Law 

2.3b Space Charge Limited Current 
2.3c Schottky Barrier 
2.3d Field Emission 

2.4 Quantum Efficiency 

2.5 Summary 


8 

9 

11 

11 

12 

14 

16 

18 

19 



3. Hole Only Diode (ITO/PEDOT/MEH-PPV/Au) 


20-32 


3.1 Hole Only Diode introduction 

3.2 Hole Only Diode Fabrication 

3.3 Role of PEDOT/PSS on Hole only devices 

3.4 PEDOT coating on an ITO-Substrate 

3.5 Barrier contact with PEDOT: PSS 

3.6 Results and Discussion: Role of PEDOT on hole only devices 

2.7a Role of PEDOT on hole only deives (YIELD) 

2.7b Advantage of using PEDOT layer in PLED 

2.7c Surface roughness 

2.7d Characterizations of Hole only devices 

3.7 Summary 


20 

21 

21 

22 

23 

25 

25 

25 

26 
26 
32 


4. Study of Electron Only Device (Mg/MEH-PP V/Ca/Al ) 33-47 

4.1 Introduction 33 

4.2 Electron only device 33 

4.3 Electron only diode fabrication 34 

4.3.1 Difficulties of coating Mg on glass 35 

4.4 Results and Discussion 37 

a. Yield of Mg on Electron only devices (Mg/MEH- 37 

PPV/Ca/Al) 


b. Nature of Electron current in Electron only device 37 

c. Characterization of Hole only and electron only device 42 

d. Results ofPLED(ITO/PEDOT/MEH-PPV/Ca/Al) device 44 


4.5 Summary 


47 



PART:-II 


5. Lift-Off process with Positive Photoresist 

5.1 Introduction to the lift-off process 

5.2 Potential of Lift-Off process in OLED/PLED cathode lines 

5.3 Lift-Off Process: Chlorobenzene soak 

5.4 Lift-Off process: Image reversal process 

5.5 Process flow chart 

5.6 The steps involved in the image reversal process 

5.7 Advantages in organic electronics 

5.8 Future Work 

5.9 Summary 

Conclusions and Future work 

Appendix A 
Appendix B 


References 


List of Figures 


Figure Page 

1 . 1 Shows Displays made of LCDs (Laptop) and OLED (flexible 1 

Plastic) 

1 1 Polymer with alternative single and double bond and the energy 3 

level in ground state. 

1 -3 Energy band diagram with frontier orbits, where x is electron 4 

affinity, Eg is the bandgap. Ip is the Ionization potential 

1 .4 Shows two different types of polarons:- hole poloran and electron 5 

poloran when excitated 

1 .5 Excitations in Organic semiconductos showing the singlet and 5 

triplet exciton, Singlets excition gives light while triplets wont. 


2. 1 (a): Simple OLED structure ITO/ MEH-PPV /Al 

8 

(b) Energy band diagram under the influence of electric field 

2.2 (a): Barrier for an intrinsic semiconductor for . 

(b) : Barrier for an intrinsic semiconductor for . 9 

(c) : Barrier for an intrinsic semiconductor for 

2.3 Ideal Characteristics of ohmic and space charge limited current. 12 

The slope of the ohmic is 1 and SCLC is 2 

2.4 Energy band diagram with Barrier lowering due to the image force 14 

where V(X) is mirror potential at distance x from contact surface 
(interface) 

2.5 Slope from FN-plot gives an indication of effective barrier height 16 

2.6 (a): Recombination Zone in single- layered device unbalanced 18 

Charge transport; (b): Balanced Charge transport 


IX 



3.1 Energy band diagram of ITO/PEDOT/MEH-PPV/Au device, 20 

cathode being gold no electron will inject into the polymer under 

the influence of electric field. 

3.2 Energy band diagram for ITO/PEDOT/MEH-PPV/Au 23 

3.3 Hole only diodes with gold as cathode 24 

3.4 Experimental J-E characteristics of ITO/PEDOT/MEH-PPV/Au 27 

hole only device in Linear-linear and log -linear scale, measured by 
Labview 7. 1 . 

3.5 Experimental J-E characteristics of ITO/PEDOT/MEH-PPV/Au 28 

. hole only device with different PEDOT thickness, log-log scale 

3.6 Fowler-Nordheim plot for ITO/PEDOT/MEH-PPV/Au, hole only 29 

device, the slop shows injection barrier height at high electric field 

3.7 Fowler-Nordheim plot for an 800 A® thick MEH-PPV, hole only 30 

device, at higher electric fields. (Zoom in of above Fig.) 

4. 1 Energy band diagram for Mg/ MEH-PPV/Ca/Al 34 

4.2 Electron only diodes with magnesium as anode and Ca/Al as anode 36 

4.3 Characteristics of Mg/MEH-PPV/Ca/Al Current Density (A/cm^) 38 

verses Electric field (V/cm) in log -linear scale 

4.4 Experimental Characteristics of Mg/MEH-PPV/Ca/Al) in log-log 39 

scale. 

4.5 Characteristics of Mg/MEH-PPV/Ca/Al Current Density (A/cm’) 40 

verses Electric field (V/cm) in log-log scale of Ca 200AVith a slop 

of 1.99. 


x 



4.6 


41 


FN-tunneling Characteristics of Mg/MEH-PPV/Ca/Al of different 
Ca thickness 

4.7 FN-tunneling for above device (i.e. 200A^ Ca thick) shows barrier 4 1 

height of 0.86eV, the knee in the curve is around 3.5 V. 

4.8 J-E Characteristics of both devices i.e. hole only device and 42 

electron only device 

4.8 J-E Characteristics of both devices i.e. hole only device and 43 

electron only device and the interpolated total current. 

4.9 Finding the electron only current, by subtracting the hole current 43 

from the PLED. The hole device and the Real device have the same 
thickness of 800 A^ and the device area is also same of 0.5 cm^ 

4. 1 0 Experimental J-E characteristics of different Ca thickness of 44 

PLED (ITO/PEDOT/MEH-PPV/Ca/Al). 

4. 1 1 FN-tunneling for all device of PEDOT 850 A® & different thickness 45 

of Ca thickness. 

4. 12 (a): Experimental J-E characteristics of PEDOT 850 A® and Ca 200 46 

A^hickness of (ITO/PEDOT/MEH-PPV/Ca/Al) 

(b) Linear fit for the 2.2 x 10^ (V/cm) (i.e. 1 .8 V) and above this 
field the current is polynomial fit. 

4. 1 3 FN-tunneling for above device (i.e PEDOT 850 A® & 200 A° Ca 47 

thick) shows barrier height of 0.04 eV, the start of field emission 

the cureve is around 2.5 V. 

5. 1 Photoresist after the lithography process 48 

(a) Normal Process (b) Positive sidewall (c) Negative sidewall 

5.2 Passive matrix display with rows as anode lines and column are as 49 

cathode lines 

5.3 Lift-Off processes in Chlorobenzene soak 50 


XI 



5.4 Reversal chemistry for the lift-Off process in image reversal 5 1 

Process 

5.5 52 
Flow chart for the process of Lift-Off using image reversal process 

5.6 Process sequence of Lift-Off positive photoresist 54 

5.7 Experimental result Lift-Off: Image reversal process. 56 

(Negativeslop) Substrate is Si and Positive Photo resist is Shipley 

1400 series (optical image) 

5.8 (a): Metal evaporation using Lift-Off image reversal process 56-7 

(b) : Metal evaporation on to the Overcut photoresist ; 

(c) : After Photoresist Lift-Off 

5.9 OLED/PLED the rib like structure is done with IR process prior to 60 

the polymer deposition. 

5.10 Soft lithography of Patterning of metal polymer 6 1 


xii 



Abbreviations and Symbols -1 


HOMO 

Highest Occupied Molecular Orbit 

LUMO 

Lowest Unoccupied Molecular Orbit 

LCD 

Liquid Crystal Display 

TFT 

Thin Film Transistor 

TV 

Television 

PC 

Personal Computer 

OLED 

Organic Light Emitting Diode 

PLED 

Polymer Light Emitting Diode 

RCA 

Radio Corporation of America 

SCLC 

Space Charge Limited Current 

FN 

Fowler-Nordheim 

ITO 

Indium Tin Oxide 

PEDOT 

Poly(3,4-€thylenedioxythiophene) 

PSS 

Poly(StyreneSulfonate) 

MEH-PPV 

poly[2-methoxy-5-(2'-ethyl-hexyloxy)- 1 ,4-phenylene vinylene] 

PPV 

Poly (Phenylene Vinylene) 

Au 

Gold 

Mg 

Magnesium 

Nd 

Neodymium 

Ca 

Calcium 

A1 

Aluminum 

Si02 

Silicon dioxide 

HCL 

Hydrochloric acid , 


xiii 



HNOb 

Nitric acid 

NH4OH 

Sulfuric acid 

Si 

Silicon 

DI 

De Ionized Water 

NH4OH 

Ammonium Hydroxide 

H2O2 

Hydrogen Peroxide 

PPR 

Positive Photo Resist 

PAC 

Photo Active Compound 

IR 

Image Reversal 

VLSI 

Very Large Scale Integration 

UV 

Ultra Violet 

PR 

Photo Resist 

PANI 

Poly Aniline 

- . DUT 

Device Under Test 


XIV 



PHYSICAL CONSTANTS 


Constant 

Symbol 

SI Units 

Other Units and/or 
Comments 

Electron volt 

eV 

1.602 X 10*'® J 

— 

Electron mass 

me 

9.110 X 10'^' kg 

511.1 KV/c^ 

Proton mass 

nip 

1.673 X 10-2’ kg 

938.3 MeV/c^ 

Neutron mass 

mn 

1.674X 10'^’ kg 

939.6 MeV/c^ 

Unified mass unit 

u 

1.661 X 10-2’ kg 

931.5 MeV/c^ 

Elementary charge 

e 

1.602 xio '^C 

— 

Planck's constant 

h 

6.626 X lO’^'* J-s 

4.136 X lO'** eV-s 

Planck's constant /(2;r) 

h/lTt 

1.054 X 10'^ J s 

6.582 X lO-'^^eV-s 

Planck's constant • c 

he 

— 

1240 eV-nm 

Planck's constant 

h 

6.626X 10'^" Js 

4.136 X 10''^ eV-s 

pi 

n 

3.142 

• 

Coulomb's law 
constant 

MiAne^ 

8.988 X lo’N-m^/C^ 

9x lO'^N-m^/C^ 

Brightness 

nits 

Cd/m^ 


Angstrom 


O 

1 

O 

3 

lO'^cm 


XV 



CHAPTER - 1 


INTRODUCTION 


1.1 Review 

As new horizons are opening up, the advent of organic electronics has already caused a 
stir in science and technology. It is an exciting time for engineers to look into the minute 
issues of the technology and explore the new possibilities of organic electronics. OLED 
technology offers a low cost thin film large area option that exploits electroluminescence 
and uses material as cheap as plastic or glass. Polymer devices typically begin to generate 
light at 2-3 volts. 

While LCDs are passive devices, active matrix LCD displays controlled by an array of 
TFTs provide heightened color and brightness. But they require back lighting which 
accounts for about half of their power requirements. This is where the PLED or OLED 
devices made by placing a series of organic thin film between electrodes (conductors) 
scores big. When an electric current is applied a process called electroluminescence emits 
a bright light. Since these are self-luminous they save on the power required for 
backlighting. This makes it suitable for a wide range of applications from TV and 
advertising displays to tiny mobile phones or pocket PC screens. 



Fig 1.1; Shows Displays made of LCDs (Laptop) and OLED (flexible Plastic) 


The viewing angle of LCDs is less compared to OLEDs. Hence the properties of OLEDs 
are being exploited by display makers. 

1.2 Brief historical overview of Electroluminescence Diodes: 

The first report pertaining to electroluminescence of an organic semiconductor by Pope et 
al. goes back to 1963. They observed luminescence from single crystalline anthracene 
with a few tens of microns thick using silver electrodes and voltages being hundred volts 
with an efficiency of nearly 1%. The difficulties with respect to crystal growth and the 
large voltages required for light emission, limited the practical application of OLEDs. 
Tang et al. in 1987, revived the interest in organic EL by using evaporated thin 
amorphous films of nearly 100 nm as emissive layer, which reduced the operating 
voltages significantly to less than 10 V [3]. The first publication describing 
electroluminescence from a polymer is by Burroughness in 1990. 

Furtheimore, the LED performance was greatly improved, by means of additional 
chargCTtransport layers. Double-layer LEDs with high peak brightness and internal 
electroluminescence efficiencies up to 4% have been reported. The long-term device 
stability and device efficiencies of polymer LEDs are rapidly increasing, but 
improvements are still desired. Polymer LEDs currently has less device lifetime because 
of degradation. Another problem is the interface and contact stability, as low work 
function metals oxidize in the presence of either HiO or O 2 . The temperature stability is 
an important parameter for display applications, displays must withstand fairly wide 
range in temperature. 



1.3 Conjugated polymers as semiconducting materials 


Conjugated polymers attract much interest currently, for use as active component in 
optoelectronic applications, viz. light-emitting diodes, photodiodes, photovoltaic cells, 
thin film transistors etc. They have a backbone consisting of alternating single and — 
double bonds (figure 1.1). In Conjugated polymers, electrons are delocalized throughout 
the entire polymer and are free to move. The overlap of it bonding and it* antibonding 
molecular orbitals forms a continuous system of electron density along the backbone. 
Conjugated polymers have bandgaps in the range of 1 to 4 eV, allowing stable optical 
excitations and mobile charge carriers. The extent of this overlap (conjugation length) 
together with the bond alternation determines the HOMO-LUMO (frontier orbits) band 

gap- 



— n 

PPV 


Delocalized 

(It* ) 


Localized 

(It ) 



LUMO 

HOMO 


Fig 1.2: Polymer with alternative single and double bond and the energy level in ground 
state. 

These materials are often strongly fluorescent and emit in the range from near infrared to 
the ultraviolet. Especially PPV and soluble derivatives thereof, are of great interest, due 
to the emission in the visible region and high luminescence quantum yields. The 
wavelength of emission depends on the extent of conjugation/delocalization, and can be 
controlled by modification of the chemical stracture. This can be done by the attachment 
of additional functional groups, which alter the electronic stmcture of the conjugated 
polymer. So, light emission is possible by radiative recombination from singlet excitons 
from the HOMO-LUMO energy gap of the polymer covering the entire spectrum. 


3 



1.4 Excitations in organic semiconductors 


Normally, semiconductor material will be in its ground state. To transport charge, and/or 
emit light, the semiconductor needs excitation, and in the case of charge transport, these 
excitations also need to be mobile. 

1.4(a) Polarons and excitons 

When an electron is taken away from the HOMO or added to the LUMO of a molecule, 
the resulting molecule is termed a radical ion, namely a radical cation for positive charge, 
and radical anion for negative charge. After removal or addition of the electron, 
molecular orbitals and the positions of nuclei will respond by a relaxation to a new 
position of minimum energy. These radical ions are often culled polarons, (electron / 
hole polaron, respectively). Due to the strong coupling between the charge carrier and the 
local lattice relaxation, removing an electron looses some energy than the HOMO called 
Ionization potential Ip, and an electron joining the molecule gains some energy than the 
LUMO is called Electron affinity x- 


Vacuum Level (OeV) 


1 

■ ■■ 

k i 

r 

LUMO ^ 

k. 

L, 

/ 




A 





A 




Ip Ebinding ’ 





Eabsorsorbiion 

1 

t 

3 

r HOMO — 

1 


Fig 1.3: Energy band diagram with frontier orbits, where x is electron affinity, 
Eg is the bandgap. Ip is the Ionization potential 


4 



Fig 1.4: Shows two difTerent types of polarons:- hole poloran and electron poloran when 
excitated 


Apart from polarons, the most important excitation in an organic semiconductor is 
exciton. This can be visualized as an electron that is removed from the HOMO, but is 
positioned into the LUMO instead of being removed entirely. A typical way of transfer of 
an electron from the HOMO into the LUMO is via the absorption of a photon (shining 
light). This exciton is electrically neutral. Alternatively, an exciton can result from the 
combination of a hole and an electron polaron. Due to the mutual attraction of electron 
and hole in the exciton, and structural relaxation of the molecule, the energy difference 
between the excitonic state and the ground state is lower than the difference between Ip 
and Ea, which in turn is lower than the difference between HOMO and LUMO. This 
energy difference is known as exciton binding energy Eb. 



Fig 1.5: Excitations in Organic semiconductors showing the singlet and triplet exciton. 
Singlet excition gives light while triplets wont 


5 


There are three ways in which hole and electron spin can combine so that the resulting 
overall spin part of the wave function is symmetric under particle exchange, and has total 
spin S = 1;- namely <]•'['>,< jj, >, and 1/V2(< > + < it >). 

These excitons are called triplet excitons. The decay of Triplet exciton is a non-radiative 
process which does not give any light. Another part of spins of the wave function that is 
antisymmetic under particle exchange is, namely l/Vl ( < ti> - < it > ). and total spin 
S = 0 is called a singlet exciton. The decay of singlet exciton may be a radiative process 
which gives light. 


1.5 Summary: 

'Understanding transport in polymer light-emitting diodes (PLEDs) has been complicated 
by the presence of both electrons and holes in working devices for which complete 
analytical models do not exist. The charge injection plays an important role in the device 
performance, because device efficiency depends on how many photons are generated in 
the emissive layer. The transport of these charges depends on the mobility, electric fields 
and temperature. 


To meet the challenges of this growing technology we have to be conversant with the 
fabrication and characterization aspects of the PLEDs. So far, no adequate description of 
the J-E behavior of Polymer LEDs has been provided. In the present study, we provide 
consistent description of the J-V characteristics of MEH-PPV devices. Polymer light 
emitting diodes (PLEDs) charge injection, which is an important criterion in PLEDs, is 
studied by identifying injection current density for electrons and holes separately. By 
studying these current densities separately we can create charge balance. Using 
ITO/PEDOT for hole injection and Ca/Al for electron injection layers we find that the J-E 
characteristics are dominated by bulk-conduction properties of MEH-PPV at fields 
lO^-loW/cm. 


6 


1.6 Thesis Layout: 


In Chapter-2, the different mechanisms of charge injection and charge transport are 
studied. In Chapter-3, a number of experiments have been performed on hole only device 
by varying PEDOT on ITO/PEDOT/MEH-PPV/Au PLED. In this device with the nature 
of hole current, the role of PEDOT on interface roughness and yield is studied. Chapter- 
4, numerous experiments have been performed similar to chapter 3 for the nature of 
electron current by varying calcium thickness in the Mg/MEH-PPV/Ca/Al PLEDs device. 
In addition single layer devices have been fabricated to study the nature of electron 
current. We have also calculated electron current by fabricating a ITO/PEDOT/MEH- 
PPV/Ca/Al PLED and the total current in such a device is due to electron and hole 
current, once the quantity of hole cvurent is known, then the electron current can also be 
calculated with simple a subtracting of hole current from total current. Finally, Chapter 5 
concludes the thesis with an interesting topic on Tift-ofF process with positive photo 
resist process, in this chapter the utility of ribs for the cathode isolation on OLEDs is 
studied. And followed by the summary, results, and future work. 


7 



CHAPTER - II 


Physics of Charge injection and Charge Transport 


2.1 General Introduction of OLED 

PLED/OLED is an electronic device that emits light when a potential is applied to the 
electrodes. A fluorescent polymer is sandwiched between the anode and the cathode. The 
anode is typically Indium-Tin Oxide (ITO), which is transparent and allows light to 
escape. On top of ITO, an emissive polymer layer is deposited, followed by a layer of 
Aluminum (Al) which acts as cathode. 



Fig 2.1: (a) 



Fig 2.1 :(a) Simple PLED structure ITO/ MEH-PPV /Al 

(b) Energy band diagram under the influence of electric field 


For a PLED to function, both the holes and electrons are required, from the anode and 
cathode respectively. The objective of the present chapter is to understand the injection 
and transport of these charge carriers. 


8 




2.2: Interface barrier & Charge Injection 

Three different types of contacts are described for a metal — semiconductor (intrinsic) 
contact. 

(I) When = ^s), the Fermi-levels of the metal and the semiconductor are already 
lined out, and no charge redistribution is required upon contact. This is called a neutral 
contact as in Fig 2.2(a): both the electron and hoje contact have an interfacial 
concentration of charge equal to their intrinsic free carrier concentration. 


r; 


<I>M ^ 


1 1>B 




METAL 



VACUUM 


2.2 (a) SEMICONDUCTOR 



Fig 2.2: (a): Barrier for an intrinsic semiconductor for 0s 

(b): Barrier for an intrinsic semiconductor for <^m< 0s 


(II) When the metal work-function is smaller than the semiconductor work-function 
(<Pm ^s) as shown in Fig.2.2 (b), the electrons are accumulated in the semiconductor, 
and the electron contact is ohmic, as electrons move from higher potential to lower 
potential. The hole contact is now injection limited, where 0^ = ^m-X 



Fig 2.2 (c): Barrier for an intrinsic semiconductor for (0,if> 4>s) 


9 



(Ill) When the metal work-function is larger than the semiconductor work-function 
(<Pm> ^a) as shown in Fig.2.2 (c), the electrons are depleted from the semiconductor. 
Due to the electron-depletion, the contact region cannot supply enough charge carriers to 
the bulk of the semiconductor, and the contact is called blocking or injection-limited for 
electrons. At the same time, the contact region contains excess of holes. As a result, the 
contact region can supply hole charges demanded by the bulk of the semiconductor, and 
the contact is called ohmic or bulk-limited for holes. Where = 0m-X. 

The experimental definition of contact barrier type. Ohmic contact for SCLC and 
injection limited contact for Contact Limited Current is different from the definitions of 
the Ohmic, neutral and injection limited contacts from the intrinsic semiconductor to 
organic electronics, because the Fermi level in polymers is not exactly defined. 

It is estimated from theoretical calculations that for a contact barrier of 0.2 eV the 
current is space charge limited at room temperature [6] and consequently the contact is 
Ohmic. When <p8> 0.2 eV, the current that the contact can supply is smaller than SCLC 
(at room temperature) and the current is limited by injection. As a result, from the 
experimental definition, the contact is called Injection-limited, irrespective of the 
fundamental definition, that can be either Ohmic, neutral or injection-limited, depending 
on 0M- 0s- 

Charge injection in metal is controlled by the work function only, irrespectiye of the 
electron affinity for electron injection and ionization potential for hole injection of the 
semiconductors. 

2.3 Charge transport 

In light emitting diodes drift current is combination of both currents, to maximize the 
efficiency, the hole current should be equal to the electron current. If this is ensured, 
every' hole will get an electron for recombination. But there is no analytical model which 


10 



can give necessary information to fabricate such a device. And it is not possible to 
measure the magnitude of the hole and electron currents in a PLED separately. Therefore, 
one has to fabricate two kinds of devices, viz. electron only and hole only devices 
separately such that J — Je, for electron only device and J = J*, in hole only device 
respectively. 

Now if we know the magnitude of the both current and try to optimize the currents in a 
composite device then the total current should be equal to both the currents. But this may 
not be true for the real device because the electron current try to influence the hole 
current and vice versa. 

As discussed earlier the currents need to inject into the active layer of the device, one has 
to know what sort of current is flowing, like ohmic, thermionic or tunneling. To analyse 
the J-V characteristics, we evaluated the influence of several mechanisms that are 
usually accounted in polymer devices. 

2.3(a): Ohms Law 

In an organic device the total current is given by the drift current only, if the background 
doping is nil. 

total drift 

Where J,, and Jt, are the electron current and hole current respectively. 

The drift current density is given by the following equations:- 

or 

11 


q, n, p V,L, Ppand //„ are the charge, magnitude of electrons, magnitude of holes, applied 
voltage, length, hole mobility and electron mobility. 

Current density is linearly proportional to the applied electric field. This class of 
conduction is dominating at low electric fields. 


2.3(b) Space Charge Limited Current: 


For conjugated polymers like PPV and its derivates the mobility is field dependent, and 
the maxiin'um current Jsclc can be found from a numerical calculation. For a field- 
independent mobility, where no compensation charge is present, the SCLC is directly 
given by the Mott-Gumey equation (considering the trap free) [5, 6,12]. 

9 9 

JscLC = -y = 7 (4) 

o o L 

Where Sr is the relative permittivity 
£o is the free space permittivity 
E is the electric field across the device 
L is the thickness 

p is the common Poole-Frenkel form of the field dependence of the hopping mobility for 
the free carrier is used [5,6], 


p = PQtxp^iE/ E q) (5) 


Po is the zero-field mobility 

Eo the electric-field coefficient to the mobility due to the interaction between charge 
carriers and randomly distributed permanent dipoles in semiconducting polymers [6]. 


12 


Finally the field dependent space charge current equation is given by 


, 9 

•'SCLC ~ g ^r^of^o — 



Where y is the electric field coefficient. 

The Log-Log curve gives a better understanding of the characteristics. The slope of the 
line gives constant value of 2, which specify the Space charge limited current 


Slope m(F) = 


d{Log{J)) ^2 

dilogiV)) " 



LOG(V) 


'^'os 


Fig 2.3: Ideal Characteristics of ohmic and space charge limited current. 
The slope of the ohmic is 1, and SCLC is 2. 


Vos is the onset of Space charge limited current 

There are two mechanisms for the electron (or hole) transport across a potential barrier: - 
thermonic emission (i.e. schottky emission) and Field emission (also called FN tunneling). 






2.3 (c) Schottky Barrier 


At low voltages, when the image force effect is minor, we applied the Schottky barrier 
model to describe dependence of current J on applied voltage V. Schottky model which 
assumes a well defined fixed potential barrier at the interface over which the electrons are 
thermionically emitted [32]. Using this model, with thermionic emission and diffusion of 
carriers, gives; 


J = J, 


exp(- 




-1 



3(U|C ^ 

=A / exp 




— (9) 


The barrier is lov/ered in the presence of image-charge effect by an amount A<P, where 
<Pb is the contact barrier potential, V is the applied bias, n is the ideality factor, ^4** is the 
effective Richardson constant [19]. 


Vacuum 



Fig 2.4: Energy band diagram with Barrier lowering due to the image force where 
V(X) is mirror potential at distance x from contact surface (interface) 


14 



( 10 ) 


And can be calculated by following equation 


A(i> = 


1 qE{0) 

V AtCEqSj. 


--( 11 ) 


0b is given by the barrier height lowering due to image force effect. 

For a given current density J, equations (6, 7) directly provide the boundary condition for 
the electric field (0) at the injecting contact. 


2.3(d) Field Emission: 

Field emissions is one of the earliest confirmations of electron tunneling as predicted by 
the quantum theory in the 1920’s by applying a large electric field to a cathode, it makes 
the electrons tunnel from the cathode through the potential barrier which is modified by 
the electric field into the vacuum. Field emission theory is conventional experimental 
method for studying the electronic structure of materials, such as the work function of 
metal surfaces. The well known Fowler-Nordheim theory gives an analytic dependence 
of the emission current density on the applied electric field and the work function, by 
assuming that the emitter is a free-electron-like metal. According to the theoiy the only 
controlling quantity that depends on the emission surface is the work-function [9,31]. 

It is widely used, as simple model for tunneling mechanism from a metals Fermi energy 
over a barrier into an adjacent material. In this mechanism, the effect of finite 


15 


temperature, and the image-force barrier lowering are ignored. Further more, applied 
voltage is larger the barrier voltage and only tunneling from the metal Fermi energy into 
the conduction band of semiconductor or insulator (polymer LUMO) are consider[30] , 
the Fowler-Nordheim equation can be written as: 


q^E^m 

exp( ^ — 

ZTrhm * (j>^ 3hqE 


—( 12 ) 


Where J = 1/A; Where A is the effective contact area; E is the applied electric field 
0b is the contact barrier height; q, m*,m, h are the charge, effective mass, free mass and 
plank constant respectively. 

(13) 

L 

Where Feff is the applied forward-bias voltage 
L is the separation distance between the two electrodes. ' 

Finally, current density is given by 

y = 1.55x10“^ exp(-6.86xlo’^^'^£“*) — (14) 

Where J = current density in amp/cm^; E = Electric field at surface in Volts/cm 
4>b =constant barrier height in Volts 


Logio( 



Fig 2.5: Slope from FN-plot gives an indication of effective barrier height 


16 


The slope m(E) of Log(J/E^) versus (1/E) plot of the FN- equation will be a negative 
slope at high electric fields as given below. 


Slope m(E) = 


d(}IE) 




— (15) 


or 


Slope m{E) = 


^(log 


(J/£2) 

e f 


d{\IE) 


= -6.86x1o7(i5j^^ 


— (16) 


An example of R'J-plot of equation 15, 16 is shown in Fig 2.4. 


Hence we can define Injection current efficiency is the ration of injected current to the 
SCLC 


Itij Ltd 

n = — ± 

SCLC 

rj = 1 (5C I C ) (17) 

77 < \(^Inj Ltd ') 

However the magnitudes of current of Schottky or field emissions (injection limited) are 
less when compared to the space charge limited current. Hence maximum current in an 
organic semiconductor is obtained when the injected current is space charge limited 
current (SCLC). 


However, the injection barrier height is not the only parameter that controls the charge 
transport mode, electric field, charge concentration and mobility are also part of it. At 
present the general interrelations between these main mechanisms in polymers are 
established qualitatively; nevertheless, there are still discussions about this in major 
details. 


17 



2.4 QUANTUM EFFICIENCY 


The quantum efficiency in PLEDs is affected by the nature of the material used in the 
emissive polymer and also by the device structure. The electroluminescence efficiency 
(jiei) is defined in equation no. 

Wliere tjpi is the photoluminescence efficiency depends on the emissive material, 
t],, is the singlet exciton quantum yield (often taken to be 25%), and 
rii is the charge balance efficiency(<l). 


For optimum device performance, the following three factors should be considered: 

( 1 ) Carrier injection and transport. 

(2) Formation of exciton. 

(3) Radiative recombination of exciton. 

TIius, it is very important to equalize the number of electrons and holes reaching emissive 
zone to maximize //,. 




Fig 2.6(b) 


Fig 2.6 :(a): Recombination Zone in single- layered device unbalanced Charge transport 


(b): Balanced Charge transport 


18 



Holes are highly mobile than eleetrons in conjugated polymers due to deep traps caused 
by oxidation electrons which makes them preferentially hole transports [8]. The lower 
electron mobility results in unbalanced transport and recombination close to the interface 
of the electron-injecting metal electrode, which causes excition quenching, leading to 
poor EL efficiencies. 

This can be overcome by introducing the same mobility of electron and hole, such that 
most of the recombination takes place, i.e. current balance (Jp~ at present not possible 
because of the unavailability of suitable materials, or by increasing the length of the 
polymer thickness so that the recombination does not takes place at the cathode interface, 
but the operating voltage increases. 

2.5 Summary: 

The different mechanisms of charge injection and transport have been reviewed. At low 
electric fields, the current density is linearly proportional to electric field (Voltage) in 
thermoinic emission. There are two mechanisms for the electron or hole transport across 
a potential barrier; - thermonic emission (i.e. schottky emission) and Field emission (also 
called FN tunneling). Thermonic emission is defined for fixed potential banier at the 
interface over which the electrons are thermionically emitted. In Field emission, the 
effect of finite temperature, and the image-force barrier lowering are, ignored. Further 
more, applied voltage is larger the banier voltage and only tunneling from the metal 
Fermi energy into the conduction band of semiconductor or insulator (polymer LUMO). 
For a field-independent mobility, where no compensation charge is present, the SCLC is 
used. However the magnitudes of cunent of these two mechanisms are less when 
compared to the space charge limited current. Hence maximum current in an organic 
semiconductor is obtained when the injected current is space charge limited current 
(SCLC). 


19 



CHAPTER - III 


HOLE ONLY DEVICE (ITO/PEDOT/MEH-PPV/Au) 


3.1 Hole Only Diode Introduction 

In order to investigate the hole current in a MEH-PPV device, the electron current needs 
to be suppressed. As gold has high work function, the Au cathode blocks the injection of 
electrons into MEH-PPV. In the Fig. 3.1 the energy band diagram of such a device is 
shown. In forward bias, the hole injection into MEH-PPV from the ITO/PEDOT: PSS 
electrode is studied. The hole currents are given by space-charge limited current with a 
field and temperature dependence of the hole mobility [5] and field emission current are 
given in Parker [4]. 


VACUUM (OeV) 



Op= S.leV 5.3eV 

of MEH-PPV 

PEDOT 


Fig 3.1; Energy band diagram of ITO/PEDOT/MEH-PPV/Au device, cathode being gold no 
electron will inject into the polymer under the influence of electric field. 

As Gold work function is 5.1 eV which is near the HOMO level of the MEH-PPV (5.3 
eV) it suppresses electron injection into the polymer, and it can be used as both anode and 
cathode for hole only devices. In the present study, ITO/PEDOT: PSS has been chosen as 


20 



anode because of it’s highly transparency which is a requirement for anode in PLED. ITO 
also has a very good work function of 4.8 to 5.0 eV (ozone treated). To verify the nature 
of the hole current, the role of hole injection layer PEDOT has been studied. 

3.2 Hole Only Diode Fabrication 

All samples were prepared on square glass substrates (5 cm X 5 cm) covered with a 
patterned layer of indium-tin-oxide GTO), which is transparent, so the light emitted by 
the LED can be collected. ITO has a work-function of 4.8 eV. This matches relatively 
well with the HOMO of the MEH-PPVs (5.2-5.3 eV) in order to form a nearly ohmic 
contact for the holes. Prior to spin coating of the organic layer(s) onto ITO, chemical and 
physical surface treatments were used to remove contaminants, smoothen the surface, and 
improve the ITO work function from 4.8 cFto 5 cF. The cleaning steps were as follows: 
rubbing with soap/detergent solution, rinsing with hot DI water, ultrasonic treatment in 
with DI water, spin-drying. Pattern the ITO substrates with proper enchants and define 
the pixel size with lithography or screen printing with epoxy in order to eliminate the 
edge effect (at edge there will be high electric field) finally UV-ozone treatment for 15 
fiiin. and hold for 10 min. ITO is a combination mixture of indium oxide and tin oxide, 
although it is widely used as an anode, has the disadvantage that oxygen diffuses into the 
organic active layer and contributes to the degradation of the device with time [5]. In 
order to improve the device stability and performance, a conductive and transparent layer 
of PEDOT-PSS consisting of poly (3, 4-ethylenedioxythiophene) (PEDOT) doped with 
polyslyrenesulfonate (PSS) obtained from H.C.Starch Baytron P VPCH 8000 Germany, 
was filtered and spin-coated. 

3.3 Role of PEDOT/PSS on Hole only devices 

PEDOT/PSS Poly(3, 4-ethylenedioxythiophene) doped with polystyrenesulfonate (PSS) is 
increasingly used in organic electronics because of its low band gap ( 1 .65 eV) and a 
high work function of the order of 5.1 to 5.2 eV, which qualifies it as good electrode for 


21 



hole injection into a semiconductor with some interesting properties. PEDOT is aqueous 
dispersions of the intrinsically conductive polymer, it is based on a hetero cyclic 
thiophene ring bridged by a diether, this means it has the same conjugated backbone as 
polythiophene. It can be spin coated onto a huge variety of conducting and non 
conducting substrates including glass, ITO, silicon, chromium, gold etc., which gives a 
good formation of thin film. 

Conductivity not only dependents on baking temperaturd but also on aqueous dispersions, 
the conductivity of the polymer conductor PEDOT; PSS doesn’t change much in aqueous 
dispersions. For an electroluminescent (EL) polymer needs only a low intrinsic 
conductivity. This makes them easy to process into coatings, or for multilayer film 
applications in conjunction with organic semiconductors. Also, Film thickness changes 
due to decrease in viscosity at room temperature [6]. 

3.4 PEDOT coating on an ITO-Substrate 

The use of PEDOT leads to a significantly improves overall device performance by 
smoothening of the anode surface and facilitating hole-injection. PEDOT is applied by 
common spin-coating techniques and is especially recommended for use in OLEDs and 
PLEDs due to reduced particle size and number of gel particles. 

The ITO anode is cleaned thoroughly and ozone treated for 15 minutes and held for 10 
minutes in ozone box. The thickness of the PEDOT layer coating onto ITO is determined 
by the following parameters: 

• spin speed (max. of 1500 r/wi) 

• dilution of DI water 

• Quality of the pre-conditioning of the substrate surface. 

Before the PEDOT is deposited onto an ITO surface, filtering of the PEDOT solution is 
done using a fresh syringe equipped with new 0.25 fan filter in order to remove residual 
gel particles or dried particulates. 


22 



The PEDOT solution was spread to cover the entire substrate surface. During spin- 
coating, the substrate is held by a vacuum chunk (4 cm diameter). In general, the layer- 
thickness was found to be homogeneous across the substrate, with a somewhat increased 
thickness at the edges of the substrate. Different thicknesses of PEDOT/PSS ranging 
between 200-850 ^ were coated to ascertain the role of PEDOT in hole only devices. 
After spin-coating, the PEDOT layer is dried for 90 minutes at 120° C in vacuum 
chamber. 

3.5 Barrier Contact with PEDOT: PSS 

With the Ionization potential change the barrier height decreases due to the introduction 
of PEDOT: PSS. Where A0pi = 0.2-0.3 eV (Fig 3.1) A0pi is purely depended on the 
work function or Fermi level of the Metal ITO. Energy barrier A0p] not only depend on 
work function but also on plasma or ozone treatment [8]. And A0p2 = 0.1 eV (from Fig 
3.1). The overall A0p has decreased from 0.3 eF to 0.1 eV which specifies the high rate 
of hole injection in the emissive layer. 


Evacuum 



Fig 3.2: Energy band diagram for ITO/PEDOT/MEH-PPV/Au 


A<Ppi is purely depended on the Fermi level of Metal ITO. On introduction of PEDOT 


A0i>2 will be depend only on PEDOT HOMO level & independent of ITO Ep or Ec. 

But for the organic conductor like PEDOT: PSS the Energy barrier A depend only on 

A0p]. 

The active organic layer was spin coated from MEH-PPV (Al’drich) filtered solution 
with a spin speed rates of 800 rpm in a nitrogen atmosphere. The polymer thickness 
varied around 800 measured by Alpha step 500 profiler. The coated sample was 
placed in a centrifugal spin dry for 7 min and vacuum baked for 120°C for 2 hours. The 
solvent used for MEH-PPV were 6 mg/ml solution of xylene and chloroform. The 
polymer solution was well stirred on magnetic stirrer for 24 hours and optionally heated 
at45°-60°C. 

The layer thickness was measured using a Tencor Alpha-step 500 surface profilometer. 
The gold metal for cathode was thermally evaporated on the sample inside a vacuum 
system at typically \0~^ mbar, typical -thickness 2500 A?. Diodes with different PEDOT 
thickness of 0 A*’, 200 A® 500 A^, 700 A*’, & 850 A*’ respectively vvere fabricated for 
understanding the role of PEDOT thickness on the performance of the device. 


Glass 



Fig 3.3: Hole only diodes with gold as cathode 

The samples were encapsulated with getter. The resulting sample consisted of four 
independent devices of same area of 0.5 cm'. 


24 


3.6 Results & Discussion: 

In these experiments of hole only devices with different PEDOT thickness, the main 
observation is the effect of PEDOT thickness on the yield of the devices. Our 
observations are summarized in table 3.1 and 3.2. 

3.6 (a) Role of PEDOT on hole only devices (YIELD) 

With PEDOT a conducting polymer, the yield details are given below with different 
thicknesses: 


Table 3.1 Effect of PEDOT thickness on the yield of the devices 

PEDOT 

Thickness 

No, of devices 

Fabricated 

No. of devices 

good 

No. of devices 

short 

No. of devices 

uncertain 

850 A® 

(undiluted) 

28 

22 

2 

4 

700/1*' 

16 

8 

5 

3 


12 

5 

6 

1 


20 

7 

10 

3 


3.6(b) Advantages of using PEDOT layer in PLED: 

An intermediate layer of PEDOT: PSS improves the yield, and smoothing of surface 
near the active polymer. 

[1 ] Smoothening of anode surface& facilitating hole injection. 

[2] Electric shorts in PLED devices can be reduced. 

[3] The forward current below turn on voltage in the PEDOT/MEH-PPV devices is 
comparatively lower than the MEH-PPV only devices of the l.D.Parker [4], 


25 






















3.6(C): Surface roughness: Surface roughness measured on Alfa step 500 surface 
profiler. 


Table 3.2: Effect of PEDOT on surface roughness 

PEDOT thickness 

■ Roughness 

8507’(pure) 

Up to 20 .4*' 

——j, 

Up to 40 


Up to 1 20 (ITO) 


From the table 2.1 and table 2.2 suggest that with the thicker PEDOT the yield of the 
devices is high, because the surface roughness is changed from ITO to PEDOT and the 
roughness of PEDOT is less compared to the surface roughness of ITO. Also the increase 
of PEDOT thickness the surface roughness of PEDOT will decEe.ase. Hence it is worth 
while to use thicker PEDOT for the PLEDs/OLEDs. 

3.6(d): Characterization of Hole only devices 

The experimental J-E characteristics of hole only device as a function of PEDOT: PSS 
laver different thicknesses, the current densities in Log-Linear scale are shown below in 
Fig- 2. 1 0. The devices characteristics measured by Labview 7.1. 


26 







I ITO/PEDOT/MEH-PPy/Ain 



I ELECTRU^LD ( V / cm ) | 


I ITO/PEDOT/MEH-PPV/Ain 



Fig 3.4: Experimental J-E characteristics of ITO/PEDOT/MEH-PPV/Au hole only device in 
(a) linear-linear (b) log -linear scale, measured by Labview 7.1. 

The experimental results of these devices show a small dependence of variations in the 
range between 500 to 850 A^. The current density of 200 is small compared to the 
other devices of the hole only diodes. The magnitudes of the current densities of these 
devices show almost same. 

The data shown in the top diagram on a Log - Linear scale are plotted on a Log - Log 
scale in the bottom diagram for better differentiation. This scale can predict the presence 
of space charge limited current. The experimental J-E characteristics of 
ITO/PEDOT/MEH-PPV/Au, hole only device are shown below in Fig 3.5 


27 







Fig 3.5: Experimental J-E characteristics of ITO/PEDOT/MEH-PPV/Au hole only device 
with different PEDOT thickness, in log-log scale. 

The results of the Fig 3.5, shows the linear dependence in log-log scale, which is space 
charge limited. The slopes of these curves are shown below in table 3.3. 


Table 3.3: The slope of the different PEDOT thickness based on Fig 3.5. 

Slope at Electric field(Horizontal) 

^ 

Slope 

Slope 

Slope 

PEDOT thickness | 

In the range of 
10* ~ lOUy/cm) 

In the range of 
10®- 10* (y/cm) 

In the range of 
10‘'-10*fF/ciw) 

850 /4®(undiluted) 

1.87 

2.44 

1.93 

700/4" 

1.7 

1.84 

1 

1.78 

500 

1.36 

2.12 ; 

j 

1.90 

200 /4" 

j 

1.90 

2,76 

2.4 


28 













The slopes ot the different PEDOT thicknesses shown for the low fields i.e of the similar 
dependence of the current at low fields at 10^ V/cm the current is not consistent due to 
thermionic emission, from the electric field, 10^ to 10^ V/cm the current is space charge 
region and greater than 10^ V/cm, the current is not space charge limited and the current 
is increasing more. 

To know clearly fields greater than 10^ V/cm, FN-tunneling is plotted in Fig 3.6 



Fig 3.6: Fowler-Nordheim plot for ITO/PEDOT/MEH-PPV/Au, hole only device, the slop 
shows injection barrier height at high electric field 

In Fig 3.6, FN-plot shows a negative slope at higher electric fields, suggesting the field 
emission phenomenon occurrence in all the devices of different PEDOT thicknesses. 

This field emission leads to barrier lowering, in Fig 3.6 shows the closer look of Fig 3.7, 
to find the slope and the barrier height. 


29 




FN -PLOT (ZOOM IN) ITO/PEDOT/MEH-PPV/AU 



Fig 3.7: Fowler-Nordheim plot for an SOOA® thick MEH-PPV, hole only device at higher 
electric fields. (Zoom in of above Fig.) 


The shape oiLn(J/E?) vs I/E curves from the data given in Fig 3.7, suggests a barrier for 
hole transport at the interface. The slopes of different PEDOT thicknesses show different 
slopes, and contact barrier heights are measured by high field FN-tunneling and are 
plotted in the table 3.4. In the above analysis we have ignored any effect of image force 
on the barrier shape. 


30 





r ^ble3.4:=T!liiivrvariationoM‘PKD»Or"iliiiicLiiies!5S, calculation of barrier height with slopes at 
tfielUsi greater thatn2Re6 mtthBffd — lunmneling equation no.( 6); considering the work 
rfumcMoiiorirO, FOOT aaJiilHHOWMO of MEH-PPV is 4.9 eF, 5.1 eKand 5.2 eK 
resspcoeti'vel^ 

PUDBCTtLIiickEiess 

Slli)|i oe 

Barrier height 

Measured (<De eV) 

22M 

■llJeeS 

0.147 

siiHF 

■SSJaei 

0.067 

771N/<'’ 


0.060 

afiiH/i" ' 

(Xumiilillated) 

■Btod 

0.052 


'We find tlinJt' for different PE5DQT li-idmesses (200 to 850 <Pe is varying from 
C.l 47 to 0.<.CS2Q, as showmintaBbleL.ir Fomhe thicker PEDOT i.e. in the range of.j500 A^ 
*0 850/i contact 'bainierh'.eig^ti issaia!®! compare to the thinner PEDOT of 200 A^. All 
these nieai'stte aments wenetakesnaatgijtt'jilii: fields i.e. 10^ V/cm. 

Til ns wes esslintiate that tlfce SCLLC obeserTidtib all our hole only devices arises from the fact 
that the iiuijtct^tion loarrier a^t tBie PLSDCOT— II EH-PPV interface is less than 0.15 eV. The 
results oof Paalcer [4] fo r hades or ilyviledoa was given by FN-tunneling (field emission) 
because s off lliue barrier h-cight waxsMiaiid 115 eFhigh, since their device was ITO/MEH- 
PPV/Au(Li.u notasedPTDi0ir:F?SSe)" 'IIie3e[esults depicted in this study given by Fig.3.1 1, 
thesloffe tfthe Lag (i)-Lag (£)Gl>olit ^re observe that the current density depends 
qaad iat: icaally on the -field Th Jshbeliinii iiti is characteristic for space charge limited current 
in wlnicn ctjses given by •eqaitaatioi'iiMoTS, 


31 



3.7 Summary: 


Hole only diode, the nature of current can be classified into three regions: - linear region 
where the electric field is less than 10^ V/cm, space charge region from 10^-10® (V/cm), 
and field emission region greater than 2x10® (V/cm). For high yield, PEDOT thickness 
should be high enough so that it reduces the roughness from ITO (roughness of 120 A°) to 
PEDOT (roughness of 20A°). With the introduction of PEDOT the roughness is 
dependent on PEDOT only not on ITO. By measuring the hole current in hole only 
devices we can know the magnitude of hole current flowing in a ITO/PEDOT/MEH- 
PPV/Ca/Al device. We have also shown, that an intermediate layer of PEDOT: PSS 
enhances yield of the polymer devices. The yield increases with increase in the thickness 
of the PEDOT layer. 


CHAPTER IV 


Study of Electron Only Device (Mg/MEH-PPV/Ca/Al) 


4.1 Introduction 

In order to know the nature and magnitude of electron current in a PLED, one has to 
fabricate the electron only device, and measure the current. Replacing the ITO & PEDOT 
contact in an ITO/PEDOT/MEH-PPV/Ca/Al with Mg low work function metal gives 
devices in which the carriers are almost exclusively electrons, due to the large offset 
between the work function of the anode and the HOMO level of M-EH-PPV [4, 13, 14]. 

Understanding the electron only current in a PLED is difficult because of the use of the 
low work function metals like Mg, Ca, Nd, etc., replacing ITO as anode, these metals 
gets oxidized in ambient environment witliin a few minutes. The fabrication of these 
devices is relatively more involved as compare to hole only devices. 

4.2 Electron Only Diode 

In an electron only device the carriers are electrons only and holes are insignificant. In 
order to investigate the electron current in a MEH-PPV device, the hole current needs to 
be suppressed. The low work function of Ca, Mg, or Nd electrode is expected to form a 
large barrier for injection of holes into MEH-PPV. In our experiments considering the 
convenience of evaporation and availability we have chosen Mg as the anode material. In 
the Fig.4.1, an energy band diagram of such a device is shown. In forward bias, the 
nature of electron injection into MEH-PPV from the Ca/Al electrode is studied. 




POLYMER 

Fig 4.1: Energy band diagram for Mg/ MEH-PPV/Ca/Al 

In forward bias, the electrons will be injected into the active layer of the device, while 
hole not injected due to large offset (A^>b ~ 1.64 eV) between the work function of the 
anode(3.66 eV) and the HOMO of MEH-PPV (5.3 eV). The current in this device is 
almost exclusively determined by the electrons injected at the Ca contact, the hole 
injecting contact plays no part in determining the I-V characteristics of these devices. 

4.3 Electron Only Diode Fabrication 

All samples were prepared on a soda lime glass consist of small fraction of sodium ions 
which are highly mobile, try to penetrate into the next layer, therefore the glass is covered 
with a small layer of SiOi to overcome the penetration. On the top of Si 02 layer ITO is 
coated, the ITO metal is stripped off in an etching solution of 225:60:15 ml of DI water, 
HCL, and HNO 3 (Nitric acid) at a temperature of 60-70° C for 10 minutes bath. Rinsing 
the substrates in DI water and cleaned in RCA solution to remove contaminants. The 
cleaning steps were as follows: rinsing with hot DI water, ultrasonic treatment in with DI 


34 


water and spin-drying. The samples were heated in a vacuum chamber for 30 min at 120** 

C and the Mg was thermally evaporated on to the glass plates with the metal masks. It 
was thermally evaporated by sublimation and the thickness of the Mg was 5600-8400 A°. 
Mg was not very uniform on the substrate and some times some pin holes were also 
visible. 

4.3.1 Difficulties of coating Mg on glass 

[1] The rate of deposition was not under control because it sublimes too rapidly. 

[2] It deposited on all the heated part and did not deposit on cold parts, such as glass bell 

jar 

[3] Surface roughness was too high (nearly 1000^°) 

[4] The deposition was not uniform on the substrate 

After the deposition of Mg, epoxy was screen printed (as discussed in chapter 3). MEH- 
PPV (Al’drich) solution is prepared with 6 mg/ml solution of xylene and chloroform. The 
polymer solution was well stirred on magnetic stirrer for 24 hours and optionally heated 
at 45-60’C. The MEH-PPV is coated on the Mg anode, with a spin speed rates of 600 
rpm, and with a filter under low light in order to prevent photooxidation of the organic 
layer due to presence of light and oxygen. The polymer thickness was typically 800 
measured by profilometer. The polymer coated sample was vacuum baked for 120® C for 
2 hours for solvent removal. 

The metals like Calcium, magnesium, aluminum are used as cathode in organic LEDs 
because of its low work functions in the order of 2.87 to 4.1 eV, which qualifies them as 
good electrodes for electron injection into polymer. Ca is a good conductor which is 
highly used as cathode with A1 coated on top on it. Ca has Fermi level (or work function) 
is close to LUMO of active polymer. The top-cathode was thermally evaporated at a slow 
rate on the sample inside a vacuum system at typically 1 0 mbar, because at high rate of 
evaporation the temperature of the filament in which Al was loaded will be high, so that 
the atoms form the filament will be having higher kinetic energy. These atoms with high 


35 



kinetic energy can damage the polymer; hence we keep at low evaporation rate. Ca/Al 
metal is used as cathode for electron-only diodes with different Ca thickness of 0 a‘^, 20 
A\ 50-85 A^, & 200 A^ respectively. The getters which are used for the encapsulation of 
the device are packed in a foil and heated for 2 hours at 180°-200°C in nitrogen flow for 
first 30 minutes and forming gas (85% nitrogen + 15% hydrogen) flow for the remaining 
time. These getters are the copper oxide a catalyst on activated can absorb oxygen and 
molecular seeds on activated can absorb moisture. These encapsulated devices are 
followed by the UV treatment for 20 minutes. The resulting sample consisted of four 
independent devices of same area of 0.5 cm^. Thickness measurement of cathode was 
done by crystal thickness monitor, during evaporation. 



*■ 

Mg as anode 


MEH-PPV 

DEVICE 


Fig 4.2: Electron only diodes with magnesium as anode and Ca/Al as anode. 


36 



4.4 Results & Discussion: 


4.4(a) Yield of Mg on Electron only devices (Mg/MEH-PPV/Ca/Al) 

In this experiment, as the Mg deposition was difficult, yield of these devices was poor, so 
the large no of devices were fabricated for the study. The following table 4. 1 shows the 
yield of the devices. 


Table 4.1: With Mg as anode, the yields of the devices details are given 

below for different thicknesses of Ca: 

Ca thickness 

No. of devices 

fabricated 

No. of devices 

good 

No. of devices 

short 


32 

11 

21 


28 

8 

20 


20 

9 

11 

oT’ 

16 

10 

6 


4.4(b): Nature of Electron current in Electron only device 

For the fabricated devices, the I-V characteristics have been measured using LabView 
[Appendix-A].The data acquired by Lab-View, are plotted in Origin have been shown 
below. 


37 


















MgfflflEH-PPV/Ca/AI 



r . I ■ I ■ I I I 1 1 1 1 

0.0 2.0x10* 4.0x10* 6.0x10* 8.0x10* 1.0x10® 1.2x10® 

Electric field ( V/cm) 


Fig 4.3: Characteristics of MgMEH-PPV/Ca/Al Current Density (A/cn^) verses Electric 
field (V/cm) in log -linear scale 


The current density of cathode Al (Ca=0^®) is 3 order of magnitude less in comparison to 
the smaller thickness of Ca - 20^° cathode as shown in Fig 4.3. With in the Ca thickness 
range of 20-200^° there is a 2 order of magnitude difference. As the Ca- thickness 
increases the current increases significantly, fire nature of electron current is difficult to 
understand and analyze in Log-linear scale. 

To determine the space charge limited current, the current density is proportional to the 
square of the electric field (voltage) in SCLC (i.e. JaE^). In log-log scale this becomes a 
straight line with slope 2. So can be easily determined whether the current density is 

space charge limited or not. 

For better understanding the same graph in Fig 4.3 is plotted in Log-Log scale in Fig 4.4. 


38 



Mg/MEH-PPV/Ca/AI 



Fig 4.4: Experimental Characteristics of Mg/MEH-PPV/CayAl) in log-log scale. 

Looking at graph Fig 3.4, the slope in the entire region is not constant, so we have tried to 
determine in different region. This information is summarized in table 4.2. 


Table 4.2: From the Fig 3.4 the slopes of the different devices are given belo’w as a 

function of electric fields. 

Ca thickness in 

10'‘-10^ (F/cm) 

10*-10‘’(F/cm) 

10*-l0\V/cm) 

0 

0J4 

0.82 

0.72 

20 

0.3 

1.06 

0.85 

50 

0.38 

1.14 

0.87 


0.55 

1.99 

1.19 


The nature of current density of different Ca thickness show different signature in 
different electric field region as shown in Fig 4.4. From table 4.2 the Ca thickness below 
200 the current is not space charge limited. While for Ca thickness 200 in the field 
region of 10-10* {V/cm), the current is space charge limited, the slope is around 2. For 
the electron only devices at less than 10'* (V/cm) the current is not space charge. 


39 














The device of our interest is Ca 200 because of its space charge behavior. The slope of 
this device is linear fitted with fitting parameters as shown below. 


Mg/MEH-PPV/Ca/AI 



LOG(E) (V/cm) 

Fig 4.S: -Characteristics of Mg/MEH-PPV/Ca/AI Current Density iA/cni‘) verses Electric 
field (V/cm) in log-log scale of Ca 200 A®with a slop of 1.99. 

From Fig 4.5, J-E characteristics resulting from injection at Ca contacts are well fitted by 
theory for space charge limited with reasonable values for the variation of fields. It is 
clear, that beyond a certain electric field the current density is even high than what is 
predicted by SCLC. The addition current density can be due to field emission (FN- 
tunneling) which is activated when the field crosses some threshold value. One has to 
draw FN plot to ascertain whether there is FN tunneling mechanism active or not. 


40 



Mg/MEH-PPV/Ca/AI 


FN-plot 



Fig 4.6: FN-tunneling Characteristics of Mg/MEH-PPV/Ca/AI of different Ca thickness 

From Fig 4.6, shows the FN-Plot for all the electron only devices. Here it is clear that for 
less than 200 thicknesses no FN tunneling is observed in electron only devices. For Ca 
thickness ~ 200 A^we observe that at electric field greater than 4 x 10* V/cm, there is a 
small knee is observed and current is showing the nature of FN tunneling. In Fig 4.7 to 
better understanding this region of electric field greater than 4 x 10* V/cm, it has been 

expanded. 



Fig 4.7: FN-tunneling for above device (i.e. 2004® Ca thick) shows barrier height of 0.086 eF, 
t the knee in the curve is around 3.5 F. 


41 





Using the method outlined previously (i.e. in chapter 3), the barrier height is calculated 
which comes out to be 86 meV. But the theoretical barrier height is 130 meV, as the work 
function of Ca is 2.87 eVmd LUMO level of MEH-PPV is 3 eF. 


4.4(c): Characterization of Hole only and electron only devices 

The hole current obtained by hole only device of PEDOT thickness of 850 A°a.nd electron 
current obtained by electron only device of Ca thickness of 200 A° has shown space 
charge limited current in the filed region of 10'‘tol0^ V/cm and 10^ to 4 x 10^ V/cm 
respectively as shown in Fig 3.8(a). 



Fig 4.8(a): J-E Characteristics of both devices Le. hole only device and electron only device 


The total current in a composite device can be a combination of the electron current and 
hole current as shown in Fig 4.8 (b). 


42 




LOG { J ) 




Fig 4.8(b): J-E Characteristics of both devices Le. hole only device and electron only device 
and the interpolated total current. 

Fig 4.9(a): Finding the electron only current, by subtracting the hole current from the 
PLED. The hole device and the Real device have the same thickness of 800 and 
the device area is also same of 0.5 cm^ 


Another way of knowing the electron current, is to fabricate the ITO/PEDOT/MEH- 
PPV/Ca/Al, PLED and find the total current and subtract the hole current from it as 
shown in Fig 4.9. But the fabricated total current is not equal to the sum of both the 
currents. 


Fig 4.9 (b): All the three currents shows 
that the total current is not the sum of 
electron and hole current. 



43 




This mo.hocl „r ,ub, racing the hole current fion, the total curntn, in a PLED cay not be 
acceptable. In a real device one kind of current may be influenced by the pmsence of 

charge carricra of the other kind by the chatge modulation of the electron current and 

hole current respectively. 


4.4 (d): Results of PLED (ITO/PEDOT/MEH-PPV/Ca/Al) device 

In electron only device and hole only device only one class of carriers had been flowing 
in the device. For a light output device it is necessaty to inject both the carriers from 
different electrodes. The nature of hole currents of different thickness and Calcium 
thickness of 200 are space charge limited, but for the bipolar carriers in a PLED the 

ctiirenl is not the space charge limited in these fields. 


These devices are fabricated with the PEDOT layer of 850 A’’ and different Ca thickness. 
The characteristics of these devices are shown below in Fig 4.10. 


ITO/PEDOT/MEH-PPV/Ca/AI 



Fig 4.10: Experimental J-E characteristics of different Ca thickness of PLED 
(ITO/PEDOT/MEH-PPV/Ca/Al). 


44 



These devices are giving light output from 1.8 V onwards. Without Ca the light output 
was greater than 4 volts. The nature of current of these devices is not space charge 
limited. To further investigate FN-tunneling for these devices. Fig 4.11 is plotted. The 
field emissions of different thickness are activated at different fields as shown in table 4.3. 


rrO/PEDOT/MEH-PPV/Ca/AI |En-PLOT| 



Fig 4.1 1 ; FN-tunneling for all device of PEDQT 850 A" & different thickness of Ca thickness. 


The calculated field of these devices are shown in the Table 4.3 


Table 4.3: Field emission for different calcium thickness and PEDOT of 850 A’’ as shown 

in Fig 4.11, calculated its start at fields given below. 


Calcium thickness in 

Field emission activated at field 

Voltage (V) at the start 


(V/cm) 

of field emission 

0 (i.e. Aluminum) 

5.8x lO" 

0.464 

20 

7.6 X 10“ 

0.608 

50 

7.7x10“ 

0.616 

200 

1.06 X lO"* 

0.848 


45 




LOG (J ) 


From this fable 4.3, it is clear that in a PLED (ITO/PEDOT/MEH-PPV/Ca/Al) of 
diflercnt thickness of Ca the Fhl-tunneling is occurring at very low fields (voltages) and 
as the thickness of the Ca increasing the initiate of field emission is also increasing its 
filed. 


.T0/PED0T«H.PPV/Ca/Al _ ITO/PEDOT/MEH-PPV/Ca/AI 



Fig4.i2(a) • Fig 4.12(b) 

Fig 4.12(a): ExperimeotaU-F characteristics of PEDOT 850 4* and Ca 200 4® thickness of 
(ITO/PEEKlT/MEH-PPV/Ca/Al). (b) Linear fit for the 2.2 x 10® (F/cm) (Le. 1.8 V) 
and above this field the current is polynomial fit 

In this device, at low electric fields the current densities are linear. At high voltages the 
current is not space charge limited. FN-tunneling for all these devices shown in Fig 4.1 1, 
the device of our interest is PEDOT thickness of 850 & Ca 200^4 the graphs of 

different plots are given in Fig 4. 1 2. 

The FN-tunneling for the ITO/PEDOT/MEH-PPV/Ca/Al with Ca thickness of 200 A° are 
given in Fig 4.13 the barrier height for this device is difficult to predict; it may be due to 
electrons or holes. 


46 





Log ( J/E') 



Fig 4.13: FN-tunneling for above device (i.e PEDOT 850/l*’& 200 A‘’ Ca thick) shows 
barrier height of 0.04 eF, the start of field emission the curve is around 2.5 F. 

The nature of electron current density for these PLEDs of different thickness of Ca, are 
not the space charge limited current because from the results the slopes of log-log curve 
is not equal 2, and at lower fields the current is due to leakage current . * ■ 


4.5 Summary: 

The nature of electron current in electron only devices are not the space charge limited 
nor the field emission for the Ca cathode thickness of less than 200 A^. For only Ca 
thickness of greater than or equal to 200 A^ of thickness the current is space charge 
limited in the field region of 10^ to 4 x 10^ F/cm. Beyond that the current is dominated by 
field emission. For a PLED of ITO/PEDOT/MEH-PPV/Ca/AI device the currents are 
dominated by the FN-tunneling, at low fields the currents are due to leakage or 
thermionic effects. 


47 




CHAPTER-V 


LIFT-OFF PROCESS WITH POSITIVE PHOTO RESIST 


5.1 Introduction to the Lift-Off process 

Photolithography is the optical process of transferring geometric shapes from a mask to 
the surface of a substrate. Positive resist undergoes bond breaking when exposed to light, 
while negative resist form bonds or cross-links between polymer chains under the 
exposure. To patterning the metallization of cathode for isolation between two metal lines 
there are three processes:- Metal mask, Metal etch(wet/dry) and Lift-Off . Metal or 
shadow mask works best for the large area of metal deposition since the creation of mask 
will be easier for mask designers. But as the size of the mask decreases it is difficult to 
design metal mask, hence resolution decreases. Metal etch is of two types - wet etch and 
dry etch, and comprises four ba.sic processes. Initially the metal is evaporated all over the 
substrate followed by the patterning using photoresist film. After lithography the metal is 
etched by an acid with the removal of photoresist. In its place, a rather sophisticated lift- 
off technique was developed, prior to metal deposition, photoresist is applied to the 
substrate and baked. The photoresist is patterned in such a way that it ends up beign 
negative sidewall after development. This then "shadows" the deposition of the metal 
films, resulting in much superior lift-off. 

Lift-Off process needs no etching; it inherently offers cost, density and negative sidewall 
advantages. In this thesis “Image Reversal Process” has been studied. 



Fig 5.1; Photoresist after the lithography process 

(a) Normal Process (b) Positive sidewall (c) Negative sidewall 


48 






5.2 Potential of Lift-Off process in OLED/PLED cathode lines 


Organic light emitting diodes are the heart of the passive matrix display, with an emissive 
polymer sandwiched directly between high and low work function metals. In 
PLEDs/OLEDs anodes are chosen as transparent materials and the top layers cathode are 
opaque. In a matrix display there are many pixels of OLED/PLED and cathode lines must 
be isolated with neighboring electrodes in order to reduce the shorts and cross talk such 
that each pixel will be independent on its sources. 

COLUMN I COLUMN 2 



COLUMN 1 COLUMN 2 

Fig 5.2: Passive matrix display with rows as anode lines and column are as cathode lines 

The separation of cathode lines in passive matrix displays can be done by Lift-Off - 
image reversal process, where the photoresist requires a negative slop (negative sidewall) 
in order to conform, to the metal isolation, and in OLED/PLEDs photoresist is not 
necessarily lifted off after the deposition of metal. 


49 


5.3 Lift-Off Process; Chlorobenzene soak 

Lift-Off process in chlorobenzene soak is anisotropic etch process [22], In this process it 
is difficult to control soak time and reproducibility is difficult to achieve. Use of toluene 
and chlorobenzene are hazardous. In the Fig 5.3: lift-Off using chlorobenzene soak 
process is given. 



Metal 

evaporation 



Fig 5.3: Lift-Off processes in Chlorobenzene soak 



5.4 Lift-Off process By Image reversal 


Image reversal is a chemical process by which a positive photoresist is made to behave 
like a negative photoresist. Positive photoresist (PPR) has the advantages of high contrast, 
good step coverage, and high aspect ratios. PPR is a radiation sensitive material 
consisting of three constituents, viz. 22% alkaline soluble base resin, 8% a photosensitive 
dissolution inhibitor (often called the Photosensitive or Photo-Active Compound (PAC)) 
and 70% of a carrier organic solvent. The photoactive compound in its initial state is an 
inhibitor of dissolution. Once this photoactive dissolution inhibitor is destroyed by light, 
the resin becomes soluble in the developer. 


50 






The working mechanism of positive photoresist is as follows - The PAC is a diazoketone 
which upon exposure to ultraviolet (UV) radiation generates a highly reactive 
intermediate ketone and liberates nitrogen. The ketone will react with available water to 
form an indene carboxylic acid which is now soluble and can be developed. In the above 
process the novolac-type resin is basically unchanged, and its solubility is controlled by 
the presence of either the dissolution inhibitor or enhancer. The degradation of 
dissolution enhancer can be utilized for the reversal of the resist image. 3 


In a reversal process imidazole is added to the positive photoresist. Upon UV exposure 
Imidazole, the novalak resin and PAC will change to the novalak resin and soluble acid 
(i.e. PAC changes to soluble acid). When baked the soluble acid changes to insoluble 
derivative. Now under the flood exposure (without the mask) the remaining PAC which 
was covered by mask previously will transform to a soluble acid. After development this 
creates a negative pattern on the substrate [20,21,23,24]. 




R Heat ( 105° C, 30 minutes ) 



Fig 5.4: Reversal chemistry for the lift-Off process in image reversal Process 





5l 




5.5 Process flow chart of Image ReversaI:-Lift-Off Process 



Fig 5.5: Flow chart for the process of Lift-Off using image reversal process 


* Important ** Critical 


52 























5.6 The steps involved in the image reversal process: 

(A) Mixing of imidazole 

Basic material such as imidazole or monazoline is added to the positive photoresist of 1 
to 2.5 percent weight before the spin coating on the substrate. In this experiment for 
13.126 grams of Photoresist 0.164 grams (i.e. of 1.25%) weight of imidazole is mixed. 
Imidazole takes 30 minutes to completely dissolve in photoresist. The added imidazole 
photoresist has got a shelf life time of 2-3 weeks. Imidazole is used to catalyze a reversal 
reaction (makes soluble acid to insoluble derivative) [20, 21,26]. 

(B) Cleaning of substrates 

The sub-strates (Si) are cleaned with RCA solution (1:1:5 solutions ofNRiOH, H202and 
D1 water). The substrates are immersed in solution and heated for 20 rain., the 
temperature being 70°C, followed by drying. 

(C) Photoresist coating 

Spin coating with positive photoresist with a spin speed of 1500-2500 rpm for 60 seconds 
produces uniform layers of about 2 pm on the substrate. 

(D) Soft bake 

The coated substrates were kept in the oven at a 95°C for 30 min. for soft bake. The soft 
bake removes the solvent from the photoresist. 

(E) Moisture 

The soft baked substrates were exposed to moisture for 1 5 to 60 seconds, the temperature 
of hot water being 45-50°C followed by Ultraviolet rays (local mercury lamp) for 1-2 
minutes with mask. The moisture plays a very important role in the repeatable and usable 
reversals [24,25]. 


5 


rn 



(F) Ultraviolet Exposure 

This exposure will define the actual width of the feature. The exposure transforms the 
photoactive compound into carboxylic acid. The imidizole molecule attaches itself to the 
acid forming an imidazolium carboxylate salt. 


(G) Reversal Bake 

The most critical parameter of the IR-process is reversal-bake temperature, once 
optimized it must be kept constant to ensure repeatability of the results. If IR-temperature 
is chosen too high (>130°C), the resist will thermally crosslink in the unexposed areas 
also, giving no pattern. Heating the substrates after exposure and prior to development to 
about 105°C causes the salt to decay leading to release of carbon dioxide. The resultant 
molecule is no longer an acid; in fact it is now as poorly soluble in base developer as 
unexposed photoactive compound. The exposed areas are as insoluble as the unexposed 
areas. The exposed areas contain a light-insensitive irdene derivative, while the 
unexposed areas still contain the original light-sensitive photoactive compound. 


(H) Flood Exposure 

Flood exposure or Blanket exposure (exposure with out mask) will render them soluble 
without altering the already exposed areas. Substrates were exposed to Ultraviolet rays 
(local mercury lamp) for 1-2 minutes without mask to the areas previously un-reacted, 
which when developed, create a negative image of the original mask with a perfect 
negative slop as shown in Fig 5.8(b). 

The flood exposure is absolutely uncritical as long as sufficient energy is applied 
to make the unexposed areas soluble. By this treatment a top layer with a lowered 
dissolution rate compared to the bottom layer is generated. 


54 



(I) Develop 


After the flood exposure the substrates are developed for 6-8minutes in the Shipley 312 
series positive photoresist developer, at room temperature with the dilution of 45:55 
(Developer : DI), rinsed in DI water and dried. The development parameters would be the 
most critical in the reversal process. A developer that was too concentrated, would result 
in total removal, and a formulation too dilute would not develop. There is a possibility 
that more negative sidewall develops with time (negative slop increases) when 
developing in solution. 



After 1** exposure UV with Mask 







After developing. 



Substrate 


I is the imidizole 
N is the novalic 
S is the soluble acid 
U is the Light-insensitive derivate 
(Insoluble Derivative) 

P is the Photo Active Compound 


Photoresist after exposure 



Photoresist 


Fig. 5.6: Process sequence of Lift-Off positive photoresist 


55 










Fig 5.7: Experimental result Lift-Off: Image reversal process. (Negative slop) 

Substrate is Si and Positive Photo resist is Shipley 1400 series (optical image) 

(J) Metal Evaporation 

Metal evaporation is been done in the vacuum chamber with a high vacuum less than 10'^ 
mbar, melted and then evaporated. The evaporated metal will deposit on the top of the 
photoresist and on the substrates as shown in fig.5.10 (a) below. 


Substrate 


lSSSSET 

iijixriixj 

cocoai 





Fig 5.8(a): Metal evaporation using Lift-Off image reversal process 


56 





Substrate 


Fig 5.8(c): After Photoresist Lift-Off 


After the evaporation of the material the metal deposited above the photoresist will also 
be lifted-ofFin acetone. 

5.6 Advantages in organic electronics 


After image reversal and metal deposition the photoresist is left outstripped in the case of 
organic materials. The ribs formed due to image reversal results in the necessary 
separation between metal lines. This procedure has two main advantages in organic 
electronics. First, organic materials being softer than inorganic materials won’t be 
affected by the solvents (acetone or acids) which are normally used for stripping of 
photoresist. Secondly, a process step is reduced (i.e removal of PR), which results in 
reduction of time of processing. 


57 





Fig 5.9: OLED/PLED the rib like structure is done with IR process prior to the polymer 
deposition. 

Photolithography is done prior to the deposition of the Organic/polymer film and cathode 
[30], high resolution is possible leading to large area thin film applications. The organic 
materials are inherently susceptible to damage from organic solvents which are generally 
used to remove photoresist (like acetone). Therefore, it is better if the photoresist is not 
removed. 

In this image reversal process, the photoresist can be left as such thereby avoiding a wet 
process step ultimately leading to saving of time and avoiding damage to the active 
material. The desired resist structure must be taller than the thickness of the metal to be 
evaporated in order to eliminate bridging of the metal on the substrate to the metal on top 
of the resist. The structure should have a small overhang (the top of the resist line larger 
than the bottom) so that the metal is not evaporated on the sidewalls of the photoresist, 
and yet the o\ erhang should be large enough to ensure consistent isolation. 


58 




5.8 FUTURE WORK 


SOFT LITHOGRAPHY 

Unlike most polymers, conducting polymers have the electrical and optical properties of 
metals or semiconductors. These materials are of increasing interest in microelectronics 
because they are inexpensive, flexible and easy to synthesize. 

Some of the conducting polymers have the nature of non-conducting when exposed to 
Ultra violet rays. Thus have the advantage of control over critical temperature in the Lift- 
Off process which ultimately reduces the fabrication process, cost and time. D. M. de 
Leeuw, C. M. J. Mutsaers, and M. M. J. Simenon, have demonstrated this model in all 
polymer ICs[28]. Such as Polyaniline doped with camphorsulfonic acid is dissolved in m- 
cresol. 



Polymer conductor 
( Photo sensitized polymer) 



BULK 



Fig 5.10: Soft lithography of Patterning of metal polymer 


A photo initiator, is added to this solution which is then spin-coated onto a substrate 
(such as polyimide foil). Under an inert atmosphere the film is exposed through a mask to 
deep ultraviolet (U V) radiation. Upon exposure the conducting 


59 



polyaniline is reduced to the no conducting leucoemeraldine form. The conducting PANI 
tracks are used as interconnects and as electrodes [ 26 , 27 , 28 ], 

5.9 Summary: 

Lift-off is excellent technique for the reproducibility of the patterning the thinner metals, 
as it needs no etching offers cost and density advantage. The first exposure has a strong 
effect on the negative sidewall profile and also determines the line widths. The moisture 
and the reversal bake are the only critical parameters involved in this process, can be 
overcome by the process optimization. The size of mask does not matter, hence used for 
the displays and VLSI area where the resolution matters. Soft lithography will be the 
budding technique, and become popular very soon as if we get a conducting polymer of 
N-type which will be capable of separating isolation when expose to UV. 


60 



CONCLUSSION and FUTURE WORK 


The nature of the hole current is space charge limited for the all thickness of PEDOT and 
it is also independent of PEDOT layer thickness. But only with 850 A° the yield is high, 
so in order to have high yield we have to use 850A° PEDOT only because the surface 
roughness changes from ITO-MEH-PPV interface to PEDOT-MEH-PPV interface. 

The electron current is a strong function of Ca layer thickness and reaches the SCLC 
value at a Ca layer thickness of 200A‘^. Beyond a certain value of electric field for thicker 
Ca, the effective barrier for electron is lowered and the FN-tunneling mechanism is 
activated leading to current values larger than SCLC. 

By finding the nature of electron current and hole current separately by fabricating hole- 
only and electron-only devices, then appropriate contact conditions at anode and cathode 
respectively have been found out to ensure maximum (i.e. SCLC) injection of both holes 
and electrons can be used. This information can be used to make a PLED which has 
better luminescence and optimal efficiency. 

Experiments can be designed to ensure charge balance which will lead to maximum 
efficiency. 

Lift-Off;-Image reversal process in a positive photoresit is used for the cathode isolation 
of OLEDs/PLEDs in a displays applications etc., where the utility of ribs like photoresist 
is required. 



Appendix-A 


Derivation for Space Charge Limited Current 


Both FN tunneling and Poole-Frenkel emission mechanism yield very low current 
densities with correspondingly low carrier densities. For structures where carriers can 
readily enter the insulator and freely flow through the insulator one finds that the 
resulting current and carrier densities are much higher. The density of free carrier causes 
a field gradient, which limits the current density. This situation occurs in lowly doped 
semiconductors and vacuum tubes. In organic polymers, there are no charge carriers. 
Therefore the current will be only due to drift. Starting from an expression for the drift 
current and Gauss’s law where we assume that the insulator contains no free carriers if no 
current flows. 


J = q p s (^ 1 ) 

9 _£_ (A 2 

d X s 


We can eliminate the carrier density, p, yielding: 


J 
s fl 


€ 


d s 
d X 


(A3) 


62 



Integrating this expression from 0 to x , where w assume the electric field to be zero at x 
= 0 one can obtains: 


— = s~ 

SJU 


or 



U4) 


Integrating once again from x = Otox =d with V (0) = V and V (d) = 0, 


d 

V = \e dx 
0 


\1J d 


3 n 


e fjL 3/2 


(A 5) 


From which one obtains the expression for the space-charge-limited current: 


9 g /r F 
8 d ' 


( A 6 ) 


63 



Appendix-B 


CHARACTERISATION OF ORGANIC LIGHT EMITTING 
DIODE 


Measuring the current and voltage in a Organic light emitting diodes is usually done by 
oscilloscope, but data cannot be saved. Using Source Measure Unit (SMU) it is easier to 
measure these characteristics. Normally SMU has IEEE commands to use for computer 
interface. These characteristics can be measured by software HP 4.00 and Labview and 
data can be saved. 


ANODE 


OLED 


V 


CATHODE 


Figure B-1. OLED/PLED with an applied voltage to anode and cathode 

OLED or organic light emitting diode is currently one of the major research areas for 
various applications like displays etc. Since these are made of organic materials they are 
cheap and consume less power. 


64 





BLOCK DIAGRAM 



Figure B-2: Block diagram for the characterization of OLED Using GPIB cables (IEEE) 

The Device under Test (DUT) is connected with a pair of connectors with Keithly (SMU) 
source measure unit, in order to source voltage, current and measure voltage current SMU 
supplies Voltage and measures Current. A Fiber optic cable is connected to DUT to 
measure the photo current. 

Photo detector is a sensor (transducer) measures light and supplies current, a resistor across 
this current gives a voltage which is measured by Keithly 193 DMM. This further can be 
converted to current of the photo detector. 

This data is written to CPU with the help of General-Purpose Interface Bus (GPIB). 

Like JOx - restores to factor}^ default conditions, etc. all the commands given below. 


SMU supplies voltage with a rage of 0-3v (our case) with a step of 0.1 volts linear stair 
case sueep. And data is available in terms of string. This data is read by GPIB by 


65 









SRQ.i.e (M Command). This string is converted by string subset and fowled by substring 
to differentiate Voltage and Current of the device. 

Similarly for photo current. The Photo detector is activated by some DC supply measures 
the Number of photons and converted into current. This current flows through a resistor 
which gives a measure of voltage. 

Characteristics of OLED: 

1) Applied Voltage VS OLED Current 

2) Photo current VS Applied Voltage 

3) Photo current VS OLED Current 


IEEE 488 COMMANDS USED FOR KETHLY (SMU): 

Source Measure unit commands 

IEEE 488 Bus address 18 (00 to 30) 


JOx - restores to factoiy^ default conditions 

FO, IX - Sources V measures I 

0, 0 sources V and measures I, (DC) 

0, 1 sources V and measures I, (Sweep) 
1 , 0 source 1 and measures V, (DC) 

1 , 1 sources 1 and measures V, (Sweep) 

0 Ox Select local sense 

0 1 X select remote sense 


66 



L40e-03,0x 


0 => auto 

40e-03 => compliance; max val of I (current) 

G5, 2, lx, G, items, format, lines 
5=> send both v and i 
2=> ASCII data, no prefix or suffix. 

1=> one line of sweeps data per talk 

Selects the type format and duty of o/p data transmitted over the bus. 
=> Use ASCII format and transmit both the V and I 

M2,x 

M (mask), compliance 
2=>Sweep is done 

All data taken is available for reading 
Tl, 0, 0, 0 

T (origin), in, out, sweepend 
Tl=> Trigger on 

0=> cont. input; 0=>nothing for o/p; 0=> end is disabled 


S3 

To control the integration time 20ms for our case. 

B0,0,0 

B Ivl, range, delay; lvcl=> i or v; range=>auto; delay=none ; To programe 
the dc bias operation , the non trigger sweep sre value and the T off sre value of 
pulse sweep 


67 



Q1,0.0^.0, 0.1, 0,500 

Q,start,stop, step, range, delay 
0=>auto range 

RlNl 

To enable or disable i/p and o/p trigger 
R1 start trigger. 

N 1 start immediately if 0 then stand by 

HOx 

Immediate bus trigger. To provide and immediate trigger stimulus for the IEEE 
bus. 

Photo Detector system commands 

IEEE 488 Bus address 10 

FO change to DC function 

RO disable i/p trigger and generate of o/p trigger 

S3 integration time 


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LAB VIEW — Block Diagram. 










LABVIEW— FRONT PANEL Diagram 










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